CA3067346A1 - Configurations d'ejecteur a ailettes - Google Patents

Configurations d'ejecteur a ailettes Download PDF

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Publication number
CA3067346A1
CA3067346A1 CA3067346A CA3067346A CA3067346A1 CA 3067346 A1 CA3067346 A1 CA 3067346A1 CA 3067346 A CA3067346 A CA 3067346A CA 3067346 A CA3067346 A CA 3067346A CA 3067346 A1 CA3067346 A1 CA 3067346A1
Authority
CA
Canada
Prior art keywords
vehicle
coupled
diffusing structure
convex surface
airfoil
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CA3067346A
Other languages
English (en)
Inventor
Andrei Evulet
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Jetoptera Inc
Original Assignee
Jetoptera Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US15/625,907 external-priority patent/US20170283080A1/en
Application filed by Jetoptera Inc filed Critical Jetoptera Inc
Publication of CA3067346A1 publication Critical patent/CA3067346A1/fr
Pending legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/38—Jet flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C15/00—Attitude, flight direction, or altitude control by jet reaction
    • B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • B64C3/14—Aerofoil profile
    • B64C3/141—Circulation Control Airfoils
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/36—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto having an ejector
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/08—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being continuous
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/17—Purpose of the control system to control boundary layer
    • F05D2270/173—Purpose of the control system to control boundary layer by the Coanda effect

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)

Abstract

L'invention concerne un système d'éjecteur pour propulser un véhicule. Le système comprend une structure de diffusion et un conduit accouplé à la structure de diffusion. Le conduit comprend une paroi ayant des ouvertures formées à travers celle-ci et conçues pour introduire dans la structure de diffusion un fluide primaire produit par le véhicule. Une surface portante est positionnée à l'intérieur de l'écoulement du fluide primaire à travers les ouvertures vers la structure de diffusion.
CA3067346A 2017-06-16 2018-06-15 Configurations d'ejecteur a ailettes Pending CA3067346A1 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US15/625,907 US20170283080A1 (en) 2015-09-02 2017-06-16 Winglet ejector configurations
US15/625,907 2017-06-16
PCT/US2018/037902 WO2018232340A1 (fr) 2017-06-16 2018-06-15 Configurations d'éjecteur à ailettes

Publications (1)

Publication Number Publication Date
CA3067346A1 true CA3067346A1 (fr) 2018-12-20

Family

ID=64660749

Family Applications (1)

Application Number Title Priority Date Filing Date
CA3067346A Pending CA3067346A1 (fr) 2017-06-16 2018-06-15 Configurations d'ejecteur a ailettes

Country Status (10)

Country Link
EP (2) EP3638587B1 (fr)
JP (1) JP7217272B2 (fr)
KR (1) KR20200056978A (fr)
CN (2) CN118205703A (fr)
BR (1) BR112019026384B8 (fr)
CA (1) CA3067346A1 (fr)
ES (1) ES3022937T3 (fr)
IL (2) IL271437B2 (fr)
MY (1) MY204828A (fr)
WO (1) WO2018232340A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111577657B (zh) * 2020-04-29 2021-10-29 南京工业大学 带有无源自激励扫掠射流流动控制装置的压气机叶片

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2052869A (en) 1934-10-08 1936-09-01 Coanda Henri Device for deflecting a stream of elastic fluid projected into an elastic fluid
GB844748A (en) * 1956-01-11 1960-08-17 English Electric Co Ltd Improvements in and relating to aircraft wings incorporating a power installation for propulsion
US3525474A (en) * 1968-12-09 1970-08-25 Us Air Force Jet pump or thrust augmentor
US3591087A (en) 1969-05-08 1971-07-06 Rohr Corp Apparatus for augmenting the thrust of an aircraft jet engine
US3819134A (en) * 1972-11-30 1974-06-25 Rockwell International Corp Aircraft system lift ejector
JPS5349612A (en) * 1976-10-14 1978-05-06 Petorobuichi Subuisuc Georugii Ejector engine thrust increase device
DK140426B (da) * 1976-11-01 1979-08-27 Arborg O J M Fremdriftsdyse til transportmidler i luft eller vand.
CA1100463A (fr) * 1978-11-22 1981-05-05 Frederick L. Gilbertson Traduction non-disponible
US4413782A (en) * 1980-12-18 1983-11-08 The United States Of America As Represented By The Secretary Of The Navy Jet excitation by an oscillating vane
US4448354A (en) * 1982-07-23 1984-05-15 The United States Of America As Represented By The Secretary Of The Air Force Axisymmetric thrust augmenting ejector with discrete primary air slot nozzles
US4815942A (en) * 1982-10-25 1989-03-28 Elayne P. Alperin Axially-symmetric, jet-diffuser ejector
US4666104A (en) 1985-07-22 1987-05-19 Kelber Charles C Combination lift thrust device
JP3525527B2 (ja) * 1994-12-21 2004-05-10 石川島播磨重工業株式会社 航空機エンジンのローブミキサ
US20060059891A1 (en) * 2004-09-23 2006-03-23 Honeywell International, Inc. Quiet chevron/tab exhaust eductor system
US7686257B2 (en) 2005-05-23 2010-03-30 Lockheed Martin Corporation Dual bimorph synthetic pulsator
US7937945B2 (en) * 2006-10-27 2011-05-10 Kinde Sr Ronald August Combining a series of more efficient engines into a unit, or modular units
US20160152324A1 (en) 2013-04-01 2016-06-02 California Institute Of Technology Fluidic fence for performance enhancement
US9587585B1 (en) * 2013-04-30 2017-03-07 The United States Of America As Represented By The Secretary Of The Air Force Augmented propulsion system with boundary layer suction and wake blowing
US20170283080A1 (en) * 2015-09-02 2017-10-05 Jetoptera, Inc. Winglet ejector configurations
EP4306789A3 (fr) 2015-09-02 2024-06-12 Jetoptera, Inc. Système propulsif fluidique

Also Published As

Publication number Publication date
IL271437B2 (en) 2025-02-01
IL315640A (en) 2024-11-01
CN111655580B (zh) 2024-01-16
CN111655580A (zh) 2020-09-11
BR112019026384B8 (pt) 2024-02-06
IL271437B1 (en) 2024-10-01
WO2018232340A1 (fr) 2018-12-20
EP3638587B1 (fr) 2025-01-15
CN118205703A (zh) 2024-06-18
JP7217272B2 (ja) 2023-02-02
MY204828A (en) 2024-09-18
BR112019026384B1 (pt) 2023-12-12
EP4563806A2 (fr) 2025-06-04
JP2020524116A (ja) 2020-08-13
IL271437A (en) 2020-01-30
KR20200056978A (ko) 2020-05-25
EP4563806A3 (fr) 2025-07-30
EP3638587A4 (fr) 2021-03-24
BR112019026384A2 (pt) 2020-07-21
ES3022937T3 (en) 2025-05-29
EP3638587A1 (fr) 2020-04-22

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